Zobrazeno 1 - 10
of 61
pro vyhledávání: '"H H Omar"'
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 19, Iss 4, Pp 43-57 (2020)
Recent studies related to fuel economy in air transport conducted in our country and abroad show that the use of recuperative heat exchangers in aviation gas turbine engines can significantly, by up to 20...30%, reduce fuel consumption. Until recentl
Externí odkaz:
https://doaj.org/article/385a565d1a344f46b5edf0d6c6588d65
Publikováno v:
AIP Conference Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a704e8a58ec031ae2a1b0098c3f6a7a
https://doi.org/10.1063/5.0127811
https://doi.org/10.1063/5.0127811
Improving the efficiency of aviation turboshaft engine with the recuperator in the helicopter system
Publikováno v:
AIP Conference Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4d1b3f1d8c262a512fa1490ba809600c
https://doi.org/10.1063/5.0128264
https://doi.org/10.1063/5.0128264
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 19, Iss 4, Pp 43-57 (2020)
Recent studies related to fuel economy in air transport conducted in our country and abroad show that the use of recuperative heat exchangers in aviation gas turbine engines can significantly, by up to 20...30%, reduce fuel consumption. Until recentl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1b013536ff7ed7d74e1382c192a019a2
https://doi.org/10.18287/2541-7533-2020-19-4-43-57
https://doi.org/10.18287/2541-7533-2020-19-4-43-57
Publikováno v:
Aeronautics and Aerospace Open Access Journal. 4:172-180
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3b9293786cca5dcb0f5dd1ce36541830
https://doi.org/10.15406/aaoaj.2020.04.00120
https://doi.org/10.15406/aaoaj.2020.04.00120
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 18, Iss 3, Pp 67-80 (2019)
Despite the fact that aviation gas turbine engines (GTE) have reached a high degree of sophistication, requirements for the improvement of their efficiency are constantly increasing. Reduction of specific fuel consumption and specific weight of the e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1cb43e63afc270ff16646d93c33776ae
https://journals.ssau.ru/index.php/vestnik/article/view/7455
https://journals.ssau.ru/index.php/vestnik/article/view/7455
Autor:
H. H. Omar, S. A. EL-Saadany
Publikováno v:
Journal of Food and Dairy Sciences. 9:403-409
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a79cd091b02e440e8cd14d45861c75f2
https://doi.org/10.21608/jfds.2018.36104
https://doi.org/10.21608/jfds.2018.36104
Publikováno v:
Journal of Physics: Conference Series. 1891:012008
The use of heat recovery in turbofan engines to improve their efficiency is not so obvious. Installing a recuperator behind the turbine of the main engine duct to heat the air at the entrance to the combustion chamber, on the one hand, reduces fuel c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa984b3ae961de74c80ed02230b87a30
https://doi.org/10.1088/1742-6596/1891/1/012008
https://doi.org/10.1088/1742-6596/1891/1/012008
Autor:
Ilia N. Krupenich, V. S. Kuz'michev, H H Omar, Yu A Tkachenko, Evgeniy P. Filinov, Ya A Ostapyuk
Publikováno v:
Journal of Physics: Conference Series. 1891:012011
Development of a gas turbine engine starts with optimization of the working process parameters. Turbine inlet temperature is among the most influential parameters that largely determine performance of an engine. As typical turbine inlet temperatures
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::140ce45e3fe7fc516c1364337a202700
https://doi.org/10.1088/1742-6596/1891/1/012011
https://doi.org/10.1088/1742-6596/1891/1/012011
Publikováno v:
Journal of Physics: Conference Series. 1745:012105
Improving the fuel efficiency of aircraft engines is the main global trend of modern propulsion engineering. One of the promising ways to improve fuel efficiency is the use of complex thermodynamic cycles with heat recovery of exhaust gases. An impor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8298e3321a0ed84a6bd32238710db470
https://doi.org/10.1088/1742-6596/1745/1/012105
https://doi.org/10.1088/1742-6596/1745/1/012105